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轴流压气机动态失速过程三维计算
引用本文:屠宝锋,胡骏,赵勇.轴流压气机动态失速过程三维计算[J].航空动力学报,2009,24(7):1616-1621.
作者姓名:屠宝锋  胡骏  赵勇
作者单位:南京航空航天大学能源与动力学院,南京,210016
基金项目:国家973项目(2007CB210301)
摘    要:基于三维非定常欧拉方程和三维激盘模型发展了一种用于研究轴流压气机动态失速过程的三维计算方法.利用该计算方法研究了某型高压压气机第一级的动态失速过程,并就转子总静压升特性的三种不同径向分布对失速过程的影响进行了分析.计算结果表明该方法能够反映出压气机的三维动态失速过程、失速团的三维空间结构,并能有效地表现出转子沿径向的特性变化对压气机气动稳定性的影响,而且还能够用于判断压气机的危险截面.

关 键 词:轴流压气机  旋转失速  激盘模型  危险截面  数值计算
收稿时间:7/9/2008 12:00:00 AM
修稿时间:9/1/2008 12:00:00 AM

Three-dimensional numerical research on stall inception in axial compressor
TU Bao-feng,HU Jun and ZHAO Yong.Three-dimensional numerical research on stall inception in axial compressor[J].Journal of Aerospace Power,2009,24(7):1616-1621.
Authors:TU Bao-feng  HU Jun and ZHAO Yong
Institution:College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Nanjing 210016;China
Abstract:A 3-D dynamic stall inception analysis method was developed based on the 3-D unsteady Euler equations and the 3-D actuator-disk model.The stall inception of the first stage of a high compressor was studied using this method.The compressors were designed using 3-D method,showing that the characteristics of the rotor are different in the radial direction,so three different static-to-total pressure ratios of rotor were studied in this paper,and the effects on the stall inception were investigated.The results s...
Keywords:axial compressor  rotating stall  actuator-disk model  dangerous section  numerical simulation  
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